View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 30294U 99025ZF 22223.04684490 .00000616 00000-0 20404-3 0 9995
2 30294 98.3398 242.0360 0211890 336.0843 47.0602 14.29517532810912
| Epoch (UTC): | 11 August 2022 01:07:27 |
| Eccentricity: | 0.0211890 |
| inclination: | 98.3398° |
| perigee height: | 641 km |
| apogee height: | 945 km |
| right ascension of ascending node: | 242.0360° |
| argument of perigee: | 336.0843° |
| revolutions per day: | 14.29517532 |
| mean anomaly at epoch: | 47.0602° |
| orbit number at epoch: | 81091 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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